Insulation layer on steel pistons without gallery

1. A galleryless piston comprising:

a body portion formed of steel,

said body portion including an upper wall including an undercrown surface,

said undercrown surface being exposed when viewed from an underside of said piston,

said upper wall including an upper combustion surface opposite said undercrown surface,

a ring belt depending from said upper wall and extending circumferentially around a central longitudinal axis of said piston,

a pair of pin bosses depending from said upper wall, and

a pair of skirt panels depending from said ring belt and coupled to said pin bosses,

a thermal barrier layer applied to at least a portion of said upper combustion surface and/or at least a portion of said ring belt, said thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of said steel of said body portion,

wherein said thermal barrier layer includes a ceramic material, and said ceramic material of said thermal barrier layer includes ceria in an amount of 90 to 100 wt. %, based on the total weight of said ceramic material.

2. A galleryless piston according claim 1 , wherein said ceria of said ceramic material has a thermal expansion coefficient at 21° C. ranging from 10E-6 to 11E-6 and said steel of said body portion has a thermal expansion coefficient at 21° C. ranging from 11E-6 to 14E-6.

3. A galleryless piston according claim 1 , wherein said ceramic material has thermal conductivity of less than 1 W/m·K.

4. A galleryless piston according claim 1 , wherein said thermal barrier layer has a gradient structure.

5. A galleryless piston according claim 4 , wherein said thermal barrier layer includes a metal bond material applied to said upper combustion surface and/or said ring belt, and said thermal barrier layer gradually transitions from 100 wt. % of said metal bond material to 100 wt. % ceramic material based on the total weight of said thermal barrier layer, and an uppermost portion of said thermal barrier layer is formed entirely of said ceramic material.

6. A galleryless piston according claim 5 , wherein said metal bond material includes steel or a superalloy.

7. A galleryless piston according claim 5 , wherein said metal bond material consists of metal in an amount of 100 wt. % based on the total weight of said metal bond material, said ceramic material consists of said ceramic in an amount of 100 wt. % based on the total weight of said ceramic material, and said thermal barrier layer consist only of said metal bond material and said ceramic material.

8. A galleryless piston according claim 1 , wherein said thermal barrier layer has a thickness of less than 500 microns.

9. A galleryless piston according to claim 1 , wherein said body portion is formed of a single piece of said steel, a plurality of struts couple said skirt panels to said pin bosses, said body portion presents an inner undercrown region extending along said undercrown surface and surrounded by said skirt panels and said struts and said pin bosses, a pair of undercrown pockets extend along said undercrown surface, each undercrown pocket is surrounded by one of said pin bosses and one of said skirt panels and said struts coupling said one pin boss to said one skirt panel, and said body portion does not have a cooling gallery floor or other features bounding or partially bounding a cooling gallery along said undercrown surface.

10. A galleryless piston comprising:

a body portion formed of steel,

said body portion including an upper wall including an undercrown surface,

said undercrown surface being exposed when viewed from an underside of said piston,

said upper wall including an upper combustion surface opposite said undercrown surface,

a ring belt depending from said upper wall and extending circumferentially around a central longitudinal axis of said piston,

a pair of pin bosses depending from said upper wall,

a pair of skirt panels depending from said ring belt and coupled to said pin bosses,

a thermal barrier layer applied to at least a portion of said upper combustion surface and/or at least a portion of said ring belt, said thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of said steel of said body portion,

said thermal barrier layer includes a ceramic material, and

wherein said ceramic material of said thermal barrier layer includes ceria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of said ceramic material.

11. A galleryless piston comprising:

a body portion formed of steel,

said body portion including an upper wall including an undercrown surface,

said undercrown surface being exposed when viewed from an underside of said piston,

said upper wall including an upper combustion surface opposite said undercrown surface,

a ring belt depending from said upper wall and extending circumferentially around a central longitudinal axis of said piston,

a pair of pin bosses depending from said upper wall,

a pair of skirt panels depending from said ring belt and coupled to said pin bosses,

a thermal barrier layer applied to at least a portion of said upper combustion surface and/or at least a portion of said ring belt, said thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of said steel of said body portion,

said thermal barrier layer includes a ceramic material, and

wherein said ceramic material of said thermal barrier layer includes a mixture of ceria stabilized zirconia and yttria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of said ceramic material.

12. A galleryless piston comprising:

a body portion formed of steel,

said body portion including an upper wall including an undercrown surface,

said undercrown surface being exposed when viewed from an underside of said piston,

said upper wall including an upper combustion surface opposite said undercrown surface,

a ring belt depending from said upper wall and extending circumferentially around a central longitudinal axis of said piston,

a pair of pin bosses depending from said upper wall,

a pair of skirt panels depending from said ring belt and coupled to said pin bosses,

a thermal barrier layer applied to at least a portion of said upper combustion surface and/or at least a portion of said ring belt, said thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of said steel of said body portion, and

wherein said body portion is formed of a single piece of said steel,

said steel has a thermal expansion coefficient at 21° C. ranging from 11E-6 to 14E-6,

a plurality of struts couple said skirt panels to said pin bosses,

said body portion presents an inner undercrown region extending along said undercrown surface and surrounded by said skirt panels and said struts and said pin bosses,

a pair of undercrown pockets extend along said undercrown surface,

each undercrown pocket is surrounded by one of said pin bosses and one of said skirt panels and said struts coupling said one pin boss to said one skirt panel,

said body portion does not have a cooling gallery floor or other features bounding or partially bounding a cooling gallery along said undercrown surface,

said upper combustion surface includes an annular first portion formed as a substantially planar surface extending along an outer periphery of said upper wall and a second portion forming a combustion bowl,

said second portion of said upper combustion surface has a non-planar, concave, or undulating surface that depends from said first portion,

said ring belt includes an upper land and a plurality of ring grooves for receipt of one or more corresponding piston rings,

said upper land extends from said upper combustion surface to an uppermost one of said ring grooves,

said pin bosses each have a pin bore,

said pin bores each have an uppermost surface which is concave,

said undercrown pockets are located radially outwardly of said pin bosses,

at least a portion of each undercrown pocket forms a portion of said undercrown surface,

said pin bosses and said skirt panels and said struts bound said inner undercrown region extending from a lowermost surface of said struts and said skirt panels to said undercrown surface,

at least a center portion of said undercrown surface disposed between said opposite skirt panels and said opposite pin bosses is concave when viewed from said underside of said piston,

said thermal barrier layer is applied to all of said upper combustion surface and said upper land of said ring belt,

said thermal barrier layer has a thickness of less than 500 microns,

said thermal barrier layer includes a ceramic material,

said ceramic material of said thermal barrier layer includes at least one of ceria, ceria stabilized zirconia, and a mixture of ceria stabilized zirconia and yttria stabilized zirconia in an amount of 90 to 100 wt. % based on the total weight of said ceramic material,

said ceramic material has thermal conductivity of less than 1 W/m·K,

said ceria of said ceramic material has a thermal expansion coefficient at 21° C. ranging from 10E-6 to 11E-6,

said thermal barrier layer has a gradient structure,

said thermal barrier layer includes a metal bond material applied to said upper combustion surface and said upper land,

said metal bond material includes steel or a superalloy,

said thermal barrier layer gradually transitions from 100 wt. % of said metal bond material to 100 wt. % of said ceramic material based on the total weight of said thermal barrier layer, and

an uppermost portion of said thermal barrier layer is formed entirely of said ceramic material.

13. A method of manufacturing a galleryless piston comprising:

applying a thermal barrier layer to at least a portion of an upper combustion surface and/or at least a portion of a ring belt of a body portion of a piston, the body portion of the piston being formed of steel, and the thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of the steel of the body portion, and

wherein the body portion includes an upper wall including the upper combustion surface and an undercrown surface which is exposed from an underside of the piston, the ring belt depends from the upper wall and extends circumferentially around a central longitudinal axis of the piston, a pair of pin bosses depend from the upper wall, and a pair of skirt panels depend from the ring belt and are coupled to the pin bosses,

wherein the step of applying the thermal barrier layer includes applying the thermal barrier layer to all of the upper combustion surface and to an upper land of the ring belt,

the step of applying the thermal barrier layer includes thermal spraying,

the thermal spraying step including plasma spraying or high velocity oxy-fuel (HVOF) spraying,

the thermal spraying step includes forming a gradient structure by first spraying a metal bond material in an amount of 100 wt. % and a ceramic material in an amount of 0 wt. % based on the total weight of the thermal barrier layer on the upper combustion surface, and then spraying the ceramic material in increasing amounts relative to the metal bond material until the composition of the thermal barrier layer is 100 wt. % ceramic material based on the total weight of the thermal barrier layer and an uppermost portion of the thermal barrier layer is formed entirely of the ceramic material,

the thermal spraying step includes applying the thermal barrier layer to a thickness of less than 500 microns,

the method further includes machining at least a portion of the upper combustion surface and/or the upper land to form a pocket, recess, rounded edge, and/or chamfer prior to applying the thermal barrier layer,

the method further includes providing the body portion formed of a single piece of the steel having a thermal expansion coefficient at 21° C. ranging from 11E-6 to 14E-6,

the body portion includes a plurality of struts coupling the skirt panels to the pin bosses, the body portion presents an inner undercrown region extending along the undercrown surface and surrounded by the skirt panels and the struts and the pin bosses, a pair of undercrown pockets extend along the undercrown surface, each undercrown pocket is surrounded by one of the pin bosses and one of the skirt panels and the struts coupling the one pin boss to the one skirt panel, the body portion does not have a cooling gallery floor or other features bounding or partially bounding a cooling gallery along the undercrown surface, the upper combustion surface includes an annular first portion formed as a substantially planar surface extending along an outer periphery of the upper wall and a second portion forming a combustion bowl, the second portion of the upper combustion surface has a non-planar, concave, or undulating surface that depends from the first portion, the ring belt includes a plurality of ring grooves for receipt of one or more corresponding piston rings, the upper land extends from the upper combustion surface to a first one of the ring grooves, the pin bosses each have a pin bore, the pin bores each have an uppermost surface which is concave, the undercrown pockets are located radially outwardly of the pin bosses, at least a portion of each undercrown pocket forms a portion of the undercrown surface, the pin bosses and the skirt panels and the struts bound the inner undercrown region extending from a lowermost surface of the struts and the skirt panels to the undercrown surface, at least a center portion of the undercrown surface disposed between the opposite skirt panels and the opposite pin bosses is concave when viewed from the underside of the piston,

the step of providing the body portion including forming the single piece of material by forging or casting,

the ceramic material of the thermal barrier layer includes at least one of ceria, ceria stabilized zirconia, and a mixture of ceria stabilized zirconia and yttria stabilized zirconia in an amount of 90 to 100 wt. % based on the total weight of the ceramic material, the ceramic material has thermal conductivity of less than 1 W/m·K, the ceria of the ceramic material has a thermal expansion coefficient at 2° C. ranging from 10E-6 to 11E-6, and

the metal bond material of the thermal barrier layer includes steel or a superalloy.

14. A method of manufacturing a galleryless piston comprising:

applying a thermal barrier layer to at least a portion of an upper combustion surface and/or at least a portion of a ring belt of a body portion of a piston, the body portion of the piston being formed of steel, the thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of the steel of the body portion, the thermal barrier layer including a ceramic material, and the ceramic material of the thermal barrier layer including ceria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, and

wherein the body portion includes an upper wall including the upper combustion surface and an undercrown surface which is exposed from an underside of the piston, the ring belt depends from the upper wall and extends circumferentially around a central longitudinal axis of the piston, a pair of pin bosses depend from the upper wall, and a pair of skirt panels depend from the ring belt and are coupled to the pin bosses.

15. A method of manufacturing a galleryless piston comprising:

applying a thermal barrier layer to at least a portion of an upper combustion surface and/or at least a portion of a ring belt of a body portion of a piston, the body portion of the piston being formed of steel, the thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of the steel of the body portion, the thermal barrier layer including a ceramic material, and the ceramic material of the thermal barrier layer including a mixture of ceria stabilized zirconia and yttria stabilized zirconia in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, and

wherein the body portion includes an upper wall including the upper combustion surface and an undercrown surface which is exposed from an underside of the piston, the ring belt depends from the upper wall and extends circumferentially around a central longitudinal axis of the piston, a pair of pin bosses depend from the upper wall, and a pair of skirt panels depend from the ring belt and are coupled to the pin bosses.

16. A method of manufacturing a galleryless piston comprising:

applying a thermal barrier layer to at least a portion of an upper combustion surface and/or at least a portion of a ring belt of a body portion of a piston, the body portion of the piston being formed of steel, the thermal barrier layer having a thermal conductivity which is lower than a thermal conductivity of the steel of the body portion, the thermal barrier layer including a ceramic material, and the ceramic material of the thermal barrier layer including ceria in an amount of 90 to 100 wt. %, based on the total weight of the ceramic material, and

wherein the body portion includes an upper wall including the upper combustion surface and an undercrown surface which is exposed from an underside of the piston, the ring belt depends from the upper wall and extends circumferentially around a central longitudinal axis of the piston, a pair of pin bosses depend from the upper wall, and a pair of skirt panels depend from the ring belt and are coupled to the pin bosses.

17. A method according to claim 16 , wherein the step of applying the thermal barrier layer includes spraying, plating, or casting.

18. A method according to claim 17 , wherein the step of applying the thermal barrier layer includes thermal spraying.

19. A method according to claim 18 , wherein the thermal spraying step includes plasma spraying or high velocity oxy-fuel (HVOF) spraying.